# N752DH: 1981 Boeing 727-223

- Status: Valid registration
- Airframe: [Boeing 727-223](https://openairdocs.org/model/boeing-727-223) (registry code 1384074, 134 seats)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 22466
- Year built: 1981
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: January 16, 2013
- Expires: January 31, 2029
- Mode S code: AA21CA
- Registered owner: [Kalitta Charters II LLC](https://openairdocs.org/faa-owner/KALITTA%20CHARTERS%20II%20LLC)
- Location: [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)
- Owner type: LLC
- Owner's area on the map: 42.2751° N, 83.5863° W: Placed by OpenAirDocs at the center of ZIP code 48198, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=752DH
- Page: https://openairdocs.org/aircraft/N752DH

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 268 in force

### Matched by airframe (Boeing 727-223)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-25-01](https://openairdocs.org/ad/2022-25-01): Wings · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 11 more. Effective Feb 16, 2023
- [AD 2021-03-09](https://openairdocs.org/ad/2021-03-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 31, 2021
- [AD 2020-06-19](https://openairdocs.org/ad/2020-06-19): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jun 22, 2020
- [AD 2019-23-04](https://openairdocs.org/ad/2019-23-04): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Feb 4, 2020
- [AD 2019-24-18](https://openairdocs.org/ad/2019-24-18): Navigation · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 11 more. Effective Feb 3, 2020
- [AD 2018-25-15](https://openairdocs.org/ad/2018-25-15): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jan 22, 2019
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-20-05](https://openairdocs.org/ad/2018-20-05): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 2 more. Effective Nov 2, 2018
- [AD 2018-17-20](https://openairdocs.org/ad/2018-17-20): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 4, 2018
- [AD 2017-19-02](https://openairdocs.org/ad/2017-19-02): Doors · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 19, 2017
- [AD 2014-21-09](https://openairdocs.org/ad/2014-21-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 3, 2014
- [AD 2014-16-09](https://openairdocs.org/ad/2014-16-09): Oxygen · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 16 more. Effective Sep 23, 2014
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-04-09](https://openairdocs.org/ad/2014-04-09): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 2, 2014
- [AD 2014-05-14](https://openairdocs.org/ad/2014-05-14): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 1, 2014
- [AD 2014-03-21](https://openairdocs.org/ad/2014-03-21): Fuselage · Boeing 727-200 Series and 727-200F Series. Effective Mar 31, 2014
- [AD 2013-24-15](https://openairdocs.org/ad/2013-24-15): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jan 8, 2014
- [AD 2013-22-03](https://openairdocs.org/ad/2013-22-03): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 5, 2013
- [AD 2013-21-07](https://openairdocs.org/ad/2013-21-07): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 5, 2013
- [AD 2013-19-08](https://openairdocs.org/ad/2013-19-08): JASC Code 3418, Stall Warning System · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 18 more. Effective Nov 6, 2013
- [AD 2013-16-17](https://openairdocs.org/ad/2013-16-17): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 27, 2013
- [AD 2013-15-15](https://openairdocs.org/ad/2013-15-15): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 20, 2013
- [AD 2013-15-11](https://openairdocs.org/ad/2013-15-11): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Sep 20, 2013
- [AD 2013-14-03](https://openairdocs.org/ad/2013-14-03): Stabilizers · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 26, 2013
- [AD 2013-14-02](https://openairdocs.org/ad/2013-14-02): Wings · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 26, 2013
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-12-05](https://openairdocs.org/ad/2011-12-05): Fuel · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jul 15, 2011
- [AD 2011-02-05](https://openairdocs.org/ad/2011-02-05): Fuselage. · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 1, 2011
- [AD 2011-01-05](https://openairdocs.org/ad/2011-01-05): Fuselage · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Feb 14, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-21-10 R1](https://openairdocs.org/ad/2009-21-10-R1): Oxygen · Airbus A300 B4-605R, A300 B4-620, A300 B4-622 and 138 more. Effective Feb 4, 2010
- [AD 2008-04-10 R1](https://openairdocs.org/ad/2008-04-10-R1): Fuel tank · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 30, 2009
- [AD 2009-20-08](https://openairdocs.org/ad/2009-20-08): Fuel system · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Nov 5, 2009
- [AD 2009-20-03](https://openairdocs.org/ad/2009-20-03): Kickboard beam · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Nov 3, 2009
- [AD 2009-20-01](https://openairdocs.org/ad/2009-20-01): Auxiliary fuel tanks · Boeing 727-200 Series with STC SA3449NM. Effective Oct 26, 2009
- [AD 2009-06-10](https://openairdocs.org/ad/2009-06-10): Lower skin and the upper fastener row of the upper skin · Boeing 727-100 Series and 727-200 Series. Effective Apr 28, 2009
- [AD 2009-05-03](https://openairdocs.org/ad/2009-05-03): Ground fault interrupter (GFI) · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Apr 3, 2009
- [AD 2008-22-12](https://openairdocs.org/ad/2008-22-12): Elevator side fitting/hinge fitting joint · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Dec 17, 2008
- [AD 2008-23-09](https://openairdocs.org/ad/2008-23-09): Insulation blanket · Boeing 727-200 Series, 727-200F Series, 737-200 Series and 18 more. Effective Dec 15, 2008
- [AD 2008-22-01](https://openairdocs.org/ad/2008-22-01): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727 Series and 17 more. Effective Nov 26, 2008
- [AD 2008-17-14](https://openairdocs.org/ad/2008-17-14): Elevator rear spar · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Oct 2, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2008-12-03](https://openairdocs.org/ad/2008-12-03): Auxiliary fuel tanks · Airbus BAC 1-11 400 Series, 707-100 Long Body, 707-100B Long Body and 15 more. Effective Jul 9, 2008
- [AD 2008-11-09](https://openairdocs.org/ad/2008-11-09): Flight deck windows · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jul 3, 2008
- [AD 2008-08-02](https://openairdocs.org/ad/2008-08-02): Main landing gear (MLG) · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective May 19, 2008

### Historical (superseded or no longer in force)

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2008-04-10](https://openairdocs.org/ad/2008-04-10) (historical): Fuel tank systems · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Mar 28, 2008
- [AD 2007-11-08](https://openairdocs.org/ad/2007-11-08) (historical): Boost pump dry bay inspection · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Jun 6, 2007
- [AD 2005-14-07](https://openairdocs.org/ad/2005-14-07) (historical): Carriage attach fittings on the foreflaps · Boeing 727-100 Series, 727-100C Series, 727-200 Series and 3 more. Effective Aug 15, 2005
- [AD 2001-24-02](https://openairdocs.org/ad/2001-24-02) (historical): Shoulder Restraint Harness Attachment · Boeing 707-100 Long Body, 707-100B Long Body, 707-300 Series (all) and 20 more. Effective Jan 4, 2002
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 95-19-08](https://openairdocs.org/ad/95-19-08) (historical): Nose Cowl · Pratt and Whitney JT8D-217A, -217C, and -219 engines, related… (Rohr STC SA4363NM). Effective Oct 20, 1995
- [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995
- [AD 86-17-05 R1](https://openairdocs.org/ad/86-17-05-R1) (historical): Frame - Cargo Door Cutout · Boeing 727-200 Series. Effective Sep 3, 1987

All 279: https://openairdocs.org/aircraft/N752DH/ads.md

## Information bulletins (advisory) (7 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006
- [SAIB NM-06-56](https://openairdocs.org/saib/NM-06-56): . Issued Jul 19, 2006

## NTSB investigations

None matched to N752DH.

## FAA accident and incident reports

None matched to N752DH.

## Service difficulty reports (115, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DHLA2008752001](https://openairdocs.org/sdr/DHLA2008752001), Nov 21, 2008: SKIN. CRACKED. NR 3 K-FLAP HAS TWO SEPARATE CRACKS AT BOTTOM CENTER JUST ABOVE BULLNOSE APPROX WS 171.5. REMOVED AND REPLACED NR 3 K-FLAP OPERATIONAL CHECK GOOD. IAW M/M 27-81
- [SDR DHLA200800127](https://openairdocs.org/sdr/DHLA200800127), Nov 15, 2008: LIGHT. MALFUNCTIONED. L1 DOOR EMERGENCY EXIT LIGHT REMAINS ON WHEN SWITCH IS IN THE OFF POSITION.
- [SDR DHLA20087521022B](https://openairdocs.org/sdr/DHLA20087521022B), Oct 22, 2008: WEDGE. DELAMINATED. RIGHT WING INBD T/E FLAP ASSY MID FLAP T/E HAS AREA OF DELAMINATION AT OUTER T/E. 337 FILED AND MP9 FILED NR 26945. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM
- [SDR DHLA20087521022A](https://openairdocs.org/sdr/DHLA20087521022A), Oct 22, 2008: WEDGE. DELAMINATED. LEFT WING INBD T/E FLAP ASSY INBD MID FLAP T/E APPROX 64 INCHES FROM OUTBOARD EDGE HAS AREA OF DELAMINATION AT PREVIOUS REPAIR. 337 FILED AND MP9 NR 26944 FILED
- [SDR DHLA200800075](https://openairdocs.org/sdr/DHLA200800075), Jun 17, 2008: BATTERY PACK. INOPERATIVE. EMERGENCY ENT LIGHTS INSIDE LIGHT INOP. REMOVED AND REPLACED BATTERIES IN LIGHT PACK, OPS CHECK GOOD IAW MM 33-50-71. FLT 119. A/C WAS GROUNDED. (A)
- [SDR DHLA200800050](https://openairdocs.org/sdr/DHLA200800050), Jun 1, 2008: ACTUATOR. LEAKING. FLIGHT 1612 ON TAKEOFF ROLL, A/C SUSTAINED HYD A-SYSTEM FAILURE PRIOR TO 60 KIAS. FOUND NR 5 KRUEGER FLAP LEAKING. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUAT
- [SDR DHL2008752511](https://openairdocs.org/sdr/DHL2008752511), Feb 26, 2008: SKIN. CRACKED. NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.
- [SDR DHL2008752609](https://openairdocs.org/sdr/DHL2008752609), Feb 26, 2008: SKIN. CRACKED. NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.
- [SDR DHL2008752509](https://openairdocs.org/sdr/DHL2008752509), Feb 23, 2008: FLAP. DELAMINATED. RT INBD MIDFLAP HAS DELAM AT LOWER OUTBD TRAILING EDGE (AT WBL 238.0). CUT OUT DELAMINATED AREA ON RT I/B MIDFLAP APPROX 1.5 INCH DIAMETER APPLIED POTTING COMPO
- [SDR DHL2008752508](https://openairdocs.org/sdr/DHL2008752508), Feb 23, 2008: RIB. CRACKED. NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727SRM 51-30-2 LOCATED, DRILLED AND DEBURRED RIB P/N 65-17
- [SDR DHL2008752606](https://openairdocs.org/sdr/DHL2008752606), Feb 23, 2008: ATTACH FITTING. CRACKED. NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-
- [SDR DHL2008752607](https://openairdocs.org/sdr/DHL2008752607), Feb 23, 2008: ATTACH FITTING. CRACKED. NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB IAW SRM 51-3
- [SDR DHL2008752506](https://openairdocs.org/sdr/DHL2008752506), Feb 8, 2008: FRAME. DENTED. AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 
- [SDR DHL2008752512](https://openairdocs.org/sdr/DHL2008752512), Feb 8, 2008: ANGLE. CRACKED. RT WING I/B L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1 HFEC VERIFIED THAT CRACK 
- [SDR DHL2008752505](https://openairdocs.org/sdr/DHL2008752505), Feb 8, 2008: FRAME. DENTED. AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 
- [SDR DHL2008752610](https://openairdocs.org/sdr/DHL2008752610), Feb 8, 2008: SPAR. CRACKED. RT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1. HFEC VERIFIED THAT C
- [SDR DHL2008752603](https://openairdocs.org/sdr/DHL2008752603), Feb 8, 2008: FRAME. DENTED. AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. 
- [SDR DHL2008752604](https://openairdocs.org/sdr/DHL2008752604), Feb 8, 2008: FRAME. DENTED. AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. 
- [SDR DHL2008752510](https://openairdocs.org/sdr/DHL2008752510), Feb 6, 2008: SKIN. DELAMINATED. LT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AIL TAB UPPER SURFACE. FABRICATED FILLER AND DOUBLER IAW B7
- [SDR DHL2008752507](https://openairdocs.org/sdr/DHL2008752507), Feb 6, 2008: STRUCTURE. CRACKED. LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HI
- [SDR DHL2008752608](https://openairdocs.org/sdr/DHL2008752608), Feb 6, 2008: SKIN. DELAMINATED. LT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AILERON. TAB UPPER SURFACE FABRICATED FILLER AND DOUBLER IA
- [SDR DHL2008752605](https://openairdocs.org/sdr/DHL2008752605), Feb 6, 2008: SKIN. CRACKED. LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HI
- [SDR DHL2008752502](https://openairdocs.org/sdr/DHL2008752502), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED
- [SDR DHL2008752504](https://openairdocs.org/sdr/DHL2008752504), Feb 4, 2008: WEB. CRACKED. LT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT 
- [SDR DHL2008752503](https://openairdocs.org/sdr/DHL2008752503), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED
- [SDR DHL2008752501](https://openairdocs.org/sdr/DHL2008752501), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED
- [SDR DHL2008752570](https://openairdocs.org/sdr/DHL2008752570), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DR
- [SDR DHL2008752550](https://openairdocs.org/sdr/DHL2008752550), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DR
- [SDR DHL2008752500](https://openairdocs.org/sdr/DHL2008752500), Feb 4, 2008: STRUCTURE. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DR
- [SDR DHL2008752602](https://openairdocs.org/sdr/DHL2008752602), Feb 4, 2008: WEB. CRACKED. LT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW SRM 51-40-2 FIG1. FABRICATED DOUBLER IAW S
- [SDR DHL2008752600](https://openairdocs.org/sdr/DHL2008752600), Feb 4, 2008: SLAT. CRACKED. RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED
- [SDR DHL2008752515](https://openairdocs.org/sdr/DHL2008752515), Feb 3, 2008: BEAM. CRACKED. RT WING T/E UPPER "J" BEAM IS CRACKED AT WBL 118. ACCOMPLISHED REPAIR TO CRACKED RT WING T/E UPPER "J" BEAM WBL 118. REPLACED MATERIAL USED J BEAM P/N BAC1506-8
- [SDR DHL2008752513](https://openairdocs.org/sdr/DHL2008752513), Feb 3, 2008: ANGLE. CRACKED. CRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8 INCHES RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W S
- [SDR DHL2008752611](https://openairdocs.org/sdr/DHL2008752611), Feb 3, 2008: ANGLE. CRACKED. CRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8" RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870
- [SDR ASTAR20070014](https://openairdocs.org/sdr/ASTAR20070014), Mar 21, 2007: SWITCH. OUT OF ADJUST. WHEN THRUST LEVERS WERE BEING ADVANCED FOR T/O NR 3 ENG THRUST REVERSER LIGHT ILLUMINATED. REJECTED T/O AT ABOUT 20 KTS. PERFORMED RTO CHECKLIST AND ABNORMAL PR
- [SDR DHL2006752004](https://openairdocs.org/sdr/DHL2006752004), Nov 29, 2006: SMOKE DETECTOR. MALFUNCTIONED. NR 5 CARGO SMOKE DETECTOR ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 5 SMOKE DETECTOR. OPS CK OF SMOKE DETECTOR SYS CKS GOOD IAW MM 26-13-00, NO EVIDENCE OF
- [SDR DHL2006752](https://openairdocs.org/sdr/DHL2006752), Aug 31, 2006: SUPPORT. CORRODED. WHILE COMPLYING WITH THE VISUAL INSPECTION OF THE UPPER WING SURFACE A BULGE WAS NOTICED JUST AFT OF THE AFT SPAR CAP AT APPROX STA 523 ON THE RIGHT WING. AFTER
- [SDR DHL2006752003](https://openairdocs.org/sdr/DHL2006752003), Jun 30, 2006: LIGHT. INOPERATIVE. L-1 EXIT LIGHT INOP. REMOVED EMERGENCY LIGHT ASSY. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSY IAW ASTAR MM 33-50-00, OPS CHECK GOOD.
- [SDR DHL2006752002](https://openairdocs.org/sdr/DHL2006752002), Mar 31, 2006: SKIN. DENTED. FOUND LEFT WING TEMP REPAIR ON LARGE DENT O/B OF INBD. LANDING LIGHT, BIRD STRIKE. REMOVED AND REPLACED L/W FIXED LEADING EDGE, FROM WS.130 TO WS.349, IAW B727 
- [SDR DHL2006752001](https://openairdocs.org/sdr/DHL2006752001), Mar 17, 2006: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING STANDBY POWER CHECK. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT ASSY. OPS CK NORMAL IAW M/M 33-50-101, P/N
- [SDR DHL2006752515](https://openairdocs.org/sdr/DHL2006752515), Jan 14, 2006: RIB. CRACKED. FOUND NR 111086; REMOVED NR 1 SLAT O/B RIB WS 720 FOR ACCESS FOUND CRACK ON RIB. REMOVED NR 1 SLAT O/B RIB WS 720 IAW B727 SRM 51-30-2 AND FABBED RIB FROM 7075-
- [SDR DHL2006752514](https://openairdocs.org/sdr/DHL2006752514), Jan 13, 2006: RIB. CRACKED. FOUND NR 111077; NR 2 SLAT, RIB NR 8 AT SLAT STA 180 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 8 SLAT 180 D
- [SDR DHL2006752513](https://openairdocs.org/sdr/DHL2006752513), Jan 13, 2006: RIB. CRACKED. FOUND NR 111076; NR 2 SLAT, RIB 7 SLAT STA 190 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB 7 SLAT STA 180 DIM 16
- [SDR DHL2006752512](https://openairdocs.org/sdr/DHL2006752512), Jan 13, 2006: SKIN. CRACKED. NR 2 SLAT RIB NR 1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 BY 5 MAT U
- [SDR DHL2006752511](https://openairdocs.org/sdr/DHL2006752511), Jan 13, 2006: HINGE. CRACKED. MCD HINGE CRACKED FROM AFT SECTION BS 650 NDT CONFIRMED. REMOVED AND REPLACED MCD AFT HINGE SECTION P/N MS20001-16-7200 PO 9002527 IAW B727 AEI M/M CHAPTER 25, 
- [SDR DHL2006572512](https://openairdocs.org/sdr/DHL2006572512), Jan 13, 2006: SLAT. CRACKED. DISCREPANCY FOUND NR 111075; NR 2 SLAT RIB NR1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLA
- [SDR DHL2006572511](https://openairdocs.org/sdr/DHL2006572511), Jan 13, 2006: HINGE. CRACKED. FOUND NR 111073; MCD HINGE CRACKED FROM AFT SECTION BS 650 NDT CONFIRMED. REMOVED AND REPLACED MCD AFT HINGE SECTION P/N MS20001-16-7200 PO 9002527 IAW AEI M/M 
- [SDR DHL2006752522](https://openairdocs.org/sdr/DHL2006752522), Jan 10, 2006: REPAIR. NONE. FOUND NR 111057; ACCOMPLISH IDENTIFICATION OF EXISTING FUSELAGE SKIN REPAIR AT BS 1155 & BETWEEN STR 29R-30R. ACCOMPLISHED IDENTIFICATION OF EXISTING FUSELAGE S
- [SDR DHL2006752521](https://openairdocs.org/sdr/DHL2006752521), Jan 10, 2006: SKIN. UNKNOWN. FOUND NR 111056; ACCOMPLISH IDENTIFICATION OF EXISTING FLUSH FUSELAGE SKIN REPAIR AT BS 499 & BETWEEN STR 19R-20R. ACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH
- [SDR DHL2006752520](https://openairdocs.org/sdr/DHL2006752520), Jan 10, 2006: REPAIR. NONE. FOUND NR 111055; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 437 & STR 18R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSEL

All 115: https://openairdocs.org/aircraft/N752DH/reports.md

## STCs that may be installed (OpenAirDocs) (837, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Boeing 727-223)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12412CH](https://openairdocs.org/stc/ST12412CH): Installation of the Dual FreeFlight Systems RA-6500 Radio Altimeter. IFL Group Inc
- [STC ST00736SE](https://openairdocs.org/stc/ST00736SE): Installation of new flight crew oxygen masks and holders. B/E Aerospace, Inc. - FSI
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST02771SE](https://openairdocs.org/stc/ST02771SE): Installation of Improved Radio Altimeter System. AeroMech Incorporated
- [STC ST02646AT](https://openairdocs.org/stc/ST02646AT): Installation of an AudioVideo In-Flight Entertainment System (IFE) per ARC Avionics Master Drawing List (MDL) ARC-VIDE-001-MDL latest FAA approved revision. ARC145 LLC
- [STC SA5040NM](https://openairdocs.org/stc/SA5040NM): Installation of cargo pallet and net. Satco Inc
- [STC ST03450AT](https://openairdocs.org/stc/ST03450AT): Installation of a horse stall system. Gregory Jackson
- [STC SA2348WE](https://openairdocs.org/stc/SA2348WE): Installation of emblem lights. The Boeing Company
- [STC ST09113AC](https://openairdocs.org/stc/ST09113AC): Installation of Tail Floodlights on Boeing 727 Engine Pylons. The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA1026NW](https://openairdocs.org/stc/SA1026NW): Installation of centerline life raft stowage compartments. Safran Cabin Inc
- [STC SA1045NW](https://openairdocs.org/stc/SA1045NW): Installation of Spacemaker I-A interior kit. Safran Cabin Inc
- [STC SA1078NW](https://openairdocs.org/stc/SA1078NW): Installation of C&D coat closet, L.H. forward unit. Safran Cabin Inc
- [STC SA1086NW](https://openairdocs.org/stc/SA1086NW): Installation of C&D coat closet, R.H. forward unit. Safran Cabin Inc
- [STC SA1174NW](https://openairdocs.org/stc/SA1174NW): Installation of a windscreen. Safran Cabin Inc
- [STC SA1305NM](https://openairdocs.org/stc/SA1305NM): Installation of coat closet, L. H. forward unit. Safran Cabin Inc
- [STC SA1306NM](https://openairdocs.org/stc/SA1306NM): Installation of coat closet, R. H. forward unit. (727-232). Safran Cabin Inc
- [STC SA1370NM](https://openairdocs.org/stc/SA1370NM): Installation of class divider-closet units and curtain header. (727-235). C & D Zodiac Inc
- [STC SA1419NM](https://openairdocs.org/stc/SA1419NM): Installation of overhead life raft stowage containers. Safran Cabin Inc
- [STC SA1442NM](https://openairdocs.org/stc/SA1442NM): Installation of Spacemaker interior kit. Safran Cabin Inc
- [STC SA1662NM](https://openairdocs.org/stc/SA1662NM): Installation of overhead stowage Quikbin retrofit kits. Safran Cabin Inc
- [STC SA2474NM](https://openairdocs.org/stc/SA2474NM): Installation of 3 coat closets and one class divider. Safran Cabin Inc
- [STC SA2480NM](https://openairdocs.org/stc/SA2480NM): Installation of divider assembly, closet assembly, cabinet assembly, coatroom assembly. Safran Cabin Inc
- [STC SA3299NM](https://openairdocs.org/stc/SA3299NM): Installation of an overhead life raft stowage compartment kit. Safran Cabin Inc. Lists 727 Series
- [STC SA3457NM](https://openairdocs.org/stc/SA3457NM): Installation of cabin divider. Safran Cabin Inc
- [STC SA469NW](https://openairdocs.org/stc/SA469NW): Installation of coat closet unit. Safran Cabin Inc
- [STC SA5169NM](https://openairdocs.org/stc/SA5169NM): Installation of Aerobin interior modification kits. Safran Cabin Inc
- [STC SA5172NM](https://openairdocs.org/stc/SA5172NM): Installation of modular lavatory components. Safran Cabin Inc
- [STC SA6051NM](https://openairdocs.org/stc/SA6051NM): Installation of Galley, G6A. Safran Cabin Inc
- [STC SA816NW](https://openairdocs.org/stc/SA816NW): Installation of spacemaker interior modification kit. Safran Cabin Inc
- [STC ST00147LA](https://openairdocs.org/stc/ST00147LA): Installation of closet and curtain header. Safran Cabin Inc
- [STC ST00577SE](https://openairdocs.org/stc/ST00577SE): Installation of SpaceLine Interior Kits. Safran Cabin Inc
- [STC ST01437LA](https://openairdocs.org/stc/ST01437LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST00556CH](https://openairdocs.org/stc/ST00556CH): Installation of a single or dual Honeywell/Trimble HT9100 Global Navigation System. Amphenol Cable and Interconnect Technologies Inc
- [STC SA3141NM](https://openairdocs.org/stc/SA3141NM): Installation of floor proximity emergency escape path. Bruce Aerospace Inc
- [STC SA2932SO](https://openairdocs.org/stc/SA2932SO): Installation of a Fairchild or Sundstrand Digital Flight Data Recorder. Acron Aviation Inc
- [STC ST00771AT](https://openairdocs.org/stc/ST00771AT): Installation of expanded parameters Digital Flight Data Recorder from 6 parameters to 24 parameters. L3 Communications/Aviation Recorders
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04515AT](https://openairdocs.org/stc/ST04515AT): Installation of Auxiliary Fuel Tank Ignition Mitigation Reticulated Polyurethane Foam in Boeing 727-223 Series. AerSale Inc
- [STC ST01395LA](https://openairdocs.org/stc/ST01395LA): Approved for model 727-100, serial number 19860 and 20279; for model 727-200, serial number 21082, 21494, and 21495. Installation of BAE Systems (formerly Canadian Marconi) Dual CMA-900 Flight Management System. Aero Technik Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST01641AT](https://openairdocs.org/stc/ST01641AT): Installation of a photoluminescent floor proximity emergency escape path marking system. STG Aerospace Inc
- [STC ST00399SE](https://openairdocs.org/stc/ST00399SE): The above boeing model which has incorporated Raisbeck Commercial Air Group Inc Master Drawing List 96B-1001, Revision D, dated September 2, 1997, or later FAA approved revision, complies iwth FAR Part 36, Stage 3 noise limits. Raisbeck Engineering Inc
- [STC ST00553SE](https://openairdocs.org/stc/ST00553SE): Incorporation of the Raisbeck Commercial Air Group inlet acoustical treatment and associated structure on certain engine nose cowls. Raisbeck Engineering Inc
- [STC ST00555SE](https://openairdocs.org/stc/ST00555SE): Modification in the leading edge slat and flap configurations. Raisbeck Engineering Inc

All 837: https://openairdocs.org/aircraft/N752DH/stcs.md

## Related

- Other Boeing 727-223 aircraft: https://openairdocs.org/model/boeing-727-223/aircraft.md

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