# Boeing 727-62C

- Type: Aircraft model (FAA registry)
- Registry code: 138402C
- Manufacturer (registry): BOEING
- Model: 727-62C
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 134
- Weight class: 20,000 lb and over
- Cruise speed: 435 mph
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-727-62c

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19850418020169I](https://openairdocs.org/incident/19850418020169I), Apr 18, 1985: Boeing 72762C (N912UP), Louisville, KY. Buzzing noise while retracting flaps and a hydraulic system failing on climb. Manually extended gear and landed.

## Service difficulty reports (136, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR UPS02239933](https://openairdocs.org/sdr/UPS02239933), Nov 25, 2002: BATTERY PACK. DISCHARGED. INSPECTION TYPE:IN BOTH EMERGENCY EXITS WILL NOT ARM. R&R BOTH BATTERY PACKS & INSTALLED NEW BATTERIES OPS CHECK GOOD.
- [SDR UPS02239250](https://openairdocs.org/sdr/UPS02239250), Sep 2, 2002: PRESSURE PANEL. CRACKED. INSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRACK CRACKED THROUGH. STOP DRILLED CRACK AS
- [SDR UPS02237405](https://openairdocs.org/sdr/UPS02237405), Jan 2, 2002: BATTERY. DISCHARGED. INSPECTION TYPE:PFLT ON PREDEPARTURE CHECK, EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOP. INSTALLED NEW BATTERIES AT COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CH
- [SDR UPS01237341](https://openairdocs.org/sdr/UPS01237341), Nov 27, 2001: SLIDE. UNSECURE. INSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY.
- [SDR UPS01237191](https://openairdocs.org/sdr/UPS01237191), Oct 26, 2001: SLIDE. UNSECURE. INSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECURED SLIDE ASSY.
- [SDR UPS01237071](https://openairdocs.org/sdr/UPS01237071), Oct 17, 2001: ACCESS PANEL. DELAMINATED. INSPECTION TYPE:C NR 1 PYLON PANEL LOWER SURFACE ACCESS PANEL 5408 HAS DELAMINATION ON UPPER SURFACE. REPAIRED IAW SRM 51-40-20.
- [SDR UPS01237058](https://openairdocs.org/sdr/UPS01237058), Oct 5, 2001: PANEL. CRACKED. INSPECTION TYPE:C RH WING, WHILE BLENDING PAINT FROM A DENT ON PANEL 65-21655-470 IT W AS NOTED THAT THE UPPER SKIN WAS CRACKED REPAIRED IAW SRM 51-40-20
- [SDR UPS01237051](https://openairdocs.org/sdr/UPS01237051), Oct 4, 2001: BEAM. CRACKED. INSPECTION TYPE:C SUSPECT CRACK IN NLG DRAGBRACE ATTACH FITTING SUPPORT BEAM IN RT AFT CORNER. REPLACEMENT OF NLG DRAGBRACE SUPPORT BEAM CARRIED OUT IAW UPS EO 
- [SDR UPS01237063](https://openairdocs.org/sdr/UPS01237063), Oct 2, 2001: STRUCTURE. CORRODED. INSPECTION TYPE:C SUSPECT CORROSION ON AFT RUDDER CONTROL QUADRANT. REPAIR CARRIED OUT IAW MM 27-20-71, 27-20-00 & DRW 65-20879.
- [SDR UPS01237046](https://openairdocs.org/sdr/UPS01237046), Oct 2, 2001: PANEL. DELAMINATED. INSPECTION TYPE:C NR 3 PYLON PANEL NR 5501 HAS DELAMINATION AT O/B FWD CORNER. REPAIRED IAW SRM.
- [SDR UPS01237039](https://openairdocs.org/sdr/UPS01237039), Oct 2, 2001: STRINGER. CORRODED. INSPECTION TYPE:C ON REMOVAL OF FLOOR PANELS FOR CABLE INSPECTION, CORROSION FOUND ON FLOOR BEAM TOP CAP BS 344 RBL6. CORROSION REMOVED IAW SRM 51-10-06, DAMAGE
- [SDR UPS01237070](https://openairdocs.org/sdr/UPS01237070), Oct 1, 2001: PANEL. DELAMINATED. INSPECTION TYPE:C NR 3 PYLON PANEL 5508 ON LOWER SURFACE HAS DELAMINATION ON LOWER SKIN. REPAIRED IAW SRM 51-40-20.
- [SDR UPS01237069](https://openairdocs.org/sdr/UPS01237069), Oct 1, 2001: SPOILER PANEL. DELAMINATED. INSPECTION TYPE:C L/H WING DELAM ON #1 SPOILER PANEL PANEL REPLACED
- [SDR UPS01237038](https://openairdocs.org/sdr/UPS01237038), Oct 1, 2001: STRINGER. CRACKED. INSPECTION TYPE:C WHILE INVESTIGATING WING SCANNING LIGHT SUSPECT CRACK STRINGER 15L F OUND CRACKED AT BS 680. DAMAGE BLENDED OUT IAW SRM 53-10-3
- [SDR UPS01237037](https://openairdocs.org/sdr/UPS01237037), Sep 30, 2001: STRINGER. CORRODED. INSPECTION TYPE:C EVIDENCE OF CORROSION ON STRINGER NESTING SECTION AT BS 440 STR24L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03
- [SDR UPS01237055](https://openairdocs.org/sdr/UPS01237055), Sep 28, 2001: STRINGER. CORRODED. INSPECTION TYPE:C SUSPECT CORROSION AT BS 1120 STR 19R AREA PAINT STRIPPED, AREA OF SUSPECT CORROSION DERIVETED, SURFACE CO RROSION AND SEALANT REMOVED BETWEEN 
- [SDR UPS01236903](https://openairdocs.org/sdr/UPS01236903), Sep 17, 2001: BRACKET. CRACKED. INSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 78-30-01
- [SDR UPS01236902](https://openairdocs.org/sdr/UPS01236902), Sep 17, 2001: STRAP. CRACKED. INSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED IAW UPS EO B727-5330-2685.
- [SDR UPS01236901](https://openairdocs.org/sdr/UPS01236901), Sep 17, 2001: TRUNNION. CORRODED. INSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CAPS. REPAIRED IAW SMRO EO 2001-044-001 UP
- [SDR UPS01236877](https://openairdocs.org/sdr/UPS01236877), Sep 17, 2001: TRUNNION. CORRODED. INSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-40-1, 
- [SDR UPS01236876](https://openairdocs.org/sdr/UPS01236876), Sep 17, 2001: DRUM. CORRODED. INSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03.
- [SDR UPS01236904](https://openairdocs.org/sdr/UPS01236904), Sep 15, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPAIRED IAW EO B727-5310-04 60.
- [SDR UPS01236890](https://openairdocs.org/sdr/UPS01236890), Sep 14, 2001: SUPPORT FITTING. CRACKED. INSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT LT NDF RT CRACK CONFIRMED ON FWD I/B UPPE
- [SDR UPS01236905](https://openairdocs.org/sdr/UPS01236905), Sep 13, 2001: SPAR. CORRODED. INSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31.
- [SDR UPS01236445](https://openairdocs.org/sdr/UPS01236445), Jul 30, 2001: BULKHEAD. CRACKED. INSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPTICLE STA 870 ****MRR FILED AS OPEN*** AI
- [SDR UPS01236432](https://openairdocs.org/sdr/UPS01236432), Jul 29, 2001: SKIN. CRACKED. INSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN***
- [SDR UPS01234964](https://openairdocs.org/sdr/UPS01234964), Feb 6, 2001: LIGHT. FAILED. INSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD.
- [SDR UPS01234653](https://openairdocs.org/sdr/UPS01234653), Jan 16, 2001: PRESSURE PANEL. CRACKED. INSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK
- [SDR UPS00232522](https://openairdocs.org/sdr/UPS00232522), Apr 30, 2000: FASTENER. CRACKED. INSPECTION TYPE:C, CRACK IN FWD CARGO DOOR CUTOUT FWD FRAME INNER FAIL-SAFE STRAP 2ND FASTENER ABOVE STR 23R LOCATED CRACKED FAIL-SAFE STRAP AT BS 522 STR 18-28
- [SDR UPS00232469](https://openairdocs.org/sdr/UPS00232469), Apr 25, 2000: CHANNEL. CORRODED. INSPECTION TYPE:C, CORROSION (C53-100-01.00-02) ON CHANNEL FROM BS 873 - BS 899 WL 188, LBL 66.5. REMOVED AND REPLACED CHANNEL PER SRM 51-40-3.
- [SDR UPS00232307](https://openairdocs.org/sdr/UPS00232307), Apr 11, 2000: LINE. BURST. INSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 2
- [SDR UPS00232243](https://openairdocs.org/sdr/UPS00232243), Apr 8, 2000: WEB. CRACKED. INSPECTION TYPE:C, WEB BENEATH STAB ACTUATED ELEV TRIM SENSOR CRACKED AT SYS A & SYS B ELEVATOR HYD LINE SUPPORT POINT (PRESS LINES). WEB REPAIRED IAW SRM 51-40
- [SDR UPS00232258](https://openairdocs.org/sdr/UPS00232258), Apr 7, 2000: FRAME. CORRODED. INSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2.
- [SDR UPS00232257](https://openairdocs.org/sdr/UPS00232257), Apr 6, 2000: STIFFENER. CORRODED. INSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REP
- [SDR UPS00232245](https://openairdocs.org/sdr/UPS00232245), Apr 6, 2000: CARGO TRACK. CRACKED. INSPECTION TYPE:C, SUSPECT CRACK FOUND ON TIE DOWN TRACK AT STA 1080, STR 28 RT ADJACENT TO FRAME CUTOUT. REPAIR CARRIED OUT IAW SRM 53-10-5.
- [SDR UPS00232244](https://openairdocs.org/sdr/UPS00232244), Apr 6, 2000: CHANNEL. CRACKED. INSPECTION TYPE:C, CRACK ON FLOOR LONGITUDINAL Z SECTION AT BS 1000 AT STR 30 IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-5 FIG 4.
- [SDR UPS00232242](https://openairdocs.org/sdr/UPS00232242), Apr 6, 2000: FRAME. CRACKED. INSPECTION TYPE:C, CRACK ON FRAME AT BS 1070 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.
- [SDR UPS00232241](https://openairdocs.org/sdr/UPS00232241), Apr 6, 2000: FRAME. CRACKED. INSPECTION TYPE:C, CRACK ON EDGE OF FRAME AT BS 1000 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.
- [SDR UPS00232256](https://openairdocs.org/sdr/UPS00232256), Apr 5, 2000: WEB. CRACKED. INSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-175
- [SDR UPS00232061](https://openairdocs.org/sdr/UPS00232061), Mar 21, 2000: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK, SECURED OPS CHECKED GOOD
- [SDR UPS99231094](https://openairdocs.org/sdr/UPS99231094), Nov 8, 1999: SUPPORT. CORRODED. INSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW MM 27-51-31.
- [SDR UPS99228532](https://openairdocs.org/sdr/UPS99228532), Jan 26, 1999: LIGHT. INOP. INSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE COCKPIT IS ON. EMERGENCY EXIT LIGHT BY FW
- [SDR UPS98228204](https://openairdocs.org/sdr/UPS98228204), Nov 9, 1998: SKIN. CORRODED. INSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1.
- [SDR UPS98228169](https://openairdocs.org/sdr/UPS98228169), Nov 4, 1998: FRAME. CRACKED. INSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 RT. REPAIRED IAW APPENDIX C OF EO B727-53
- [SDR UPS98228205](https://openairdocs.org/sdr/UPS98228205), Nov 3, 1998: SKIN. CORRODED. INSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11.
- [SDR UPS98228166](https://openairdocs.org/sdr/UPS98228166), Nov 3, 1998: FRAME. CORRODED. INSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3.
- [SDR UPS98228161](https://openairdocs.org/sdr/UPS98228161), Nov 3, 1998: BULKHEAD BEAM. CRACKED. INSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED I
- [SDR UPS98228162](https://openairdocs.org/sdr/UPS98228162), Nov 2, 1998: SUPPORT. CORRODED. INSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 51-30-2.
- [SDR UPS98228136](https://openairdocs.org/sdr/UPS98228136), Nov 2, 1998: INTERCOSTAL. DAMAGED. INSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1.
- [SDR UPS98228131](https://openairdocs.org/sdr/UPS98228131), Nov 2, 1998: BULKHEAD. DAMAGED. INSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1.

All 136: https://openairdocs.org/model/boeing-727-62c/reports.md

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