# Service difficulty reports: N748DH, cancelled Oct 31, 2017

A list on [N748DH, cancelled Oct 31, 2017](https://openairdocs.org/deregistered/N748DH-2017-10-31.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 131 reports

- [SDR DHL2008F00004](https://openairdocs.org/sdr/DHL2008F00004.md): Structure · cracked · Jul 1, 2008 · N748DH · Boeing 727225 · Leading Edge Devices
  > NON-ROUTINE 068119 LT WING NR 3 I/E SLAT AT INBOARD TRACK HAS CRACK IN SKIN AT RADIUS. THIS IS A MINOR REPAIR. STOPPED DRILLED CRACK AND INSTALLED REPAIR DOUBLER. ALL WORK ACCOMPLISHED IAW SRM 51-40-2. NON-ROUTINE 068125 LT WING NR 3 I/E SLAT AT OUTBOARD T
- [SDR DHLA200800056](https://openairdocs.org/sdr/DHLA200800056.md): Wheel · vibration · Jun 9, 2008 · N748DH · Boeing 727225 · Wheel/Ski/Float
  > RTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE & MODERATE BREAKING USED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520. AIRCRAFT WAS GROUNDED. (A)
- [SDR DHLA200800055](https://openairdocs.org/sdr/DHLA200800055.md): Wheel · noisy · Jun 9, 2008 · N748DH · Boeing 727225 · Wheel/Ski/Float
  > RTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE AND MODERATE BREAKING USED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520 AIRCRAFT WAS GROUNDED. (A)
- [SDR DHLA200800021](https://openairdocs.org/sdr/DHLA200800021.md): Fire Warning · false activation · Mar 4, 2008 · N748DH · Boeing 727225 · Fire Detection
  > DURING PUSH BACK ON GROUND, GOT INTERMITTENT FIRE BELL WARNING. FOUND LIGHT IN APU HANDLE ILLUMINATED. PERFORMED 1'S, PERFORMED CHECKLIST, CALL FIRE RESCUE AND HAD MX CHECK FOR FIRE. FIRE LIGHT IN HANDLE REMAIN ON. AS PER MAINT CONTROL APU OPERATION DEFERR
- [SDR DHL2007748034](https://openairdocs.org/sdr/DHL2007748034.md): Window Frame · corroded · Nov 2, 2007 · N748DH · Boeing 727225 · Fuselage Main, Structure
  > LT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG IAW MM 53-20-00 AND DRAWING NR AE727-1-105. CLEANED WINDOW PLUG PANE FOR EVALUATION NO CORROSION NOTED IAW S0PM 20-30-3. REMOVED CORROSION ON WINDOW FRAME. CORROSION FO
- [SDR DHL2007748033](https://openairdocs.org/sdr/DHL2007748033.md): Window Frame · corroded · Nov 2, 2007 · N748DH · Boeing 727225 · Fuselage Main, Structure
  > RIGHT WINDOW FRAME PLUG AT STATION 950F TO 970 HAS CORROSION. REMOVED WINDOW PANE AND PLUG AT BS 950F TO 970 RIGHT IAW M/M 53-20-00 FIGURE 1 AND AEI DRAWING NR AE727-1-105 REV B. REMOVED CORROSION FROM WINDOW FRAME, FOUND OUT OF LIMITS IAW SRM 51-10-6, 56-2
- [SDR DHL2007748025](https://openairdocs.org/sdr/DHL2007748025.md): Stringer · cracked · Oct 25, 2007 · N748DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > LEFT WHEEL WELL STRINGER 18A CRACKED AT BS 940. CUT OUT DAMAGED SECTION OF STRINGER 18A LEFT AFT OF STATION 940 NDT AREA IAW B-727 NDTM PT 6 51-00-00 FIGURE 23. NO CRACK BEYOND CUT OUT. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING SVC REQUEST AND REPAIR
- [SDR DHL2007748032](https://openairdocs.org/sdr/DHL2007748032.md): Skin · cracked · Oct 24, 2007 · N748DH · Boeing 727225 · Trailing Edge Flaps
  > LEFT INBOARD MID FLAP UPPER SURFACE WBL124 AT MID SPAR SKIN IS CRACKED AT LOCK FASTENER. REMOVED FASTENERS ON LEFT INBOARD MID FLAP UPPER SURFACE COMMON TO MID FLAP SPAR STA 124.2 IAW SRM 51-30-2. C/W HFEC IAW NDT PT 6 51-00-00 FIGURE 23, ALUMINUM PART SURFA
- [SDR DHL2007748001](https://openairdocs.org/sdr/DHL2007748001.md): Bulkhead · cracked · Oct 22, 2007 · N748DH · Boeing 727225 · Fuselage Main, Bulkhead
  > RIGHT WW BS 870 BELOW LEAD CONTROL VALVE, BULKHEAD HAS 2 INCH CRACK. CUT OUT DAMAGED AREA BELOW APU LEAD CONTROL, CUT OUT 2" BY.75". FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-9 FIGURE 5. HEAT TREATED TO 150-190 KSI PER SPEC PO NR 7307279. AL
- [SDR DHL2007748028](https://openairdocs.org/sdr/DHL2007748028.md): Frame · dented · Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > REWORK DUE TO IMPROPER REPAIR FRAME AT 9G BARRIER BS 348.2 IS DENTED BETWEEN STRINGER 5L AND STRINGER 6L. REMOVED SRM REPAIR AT FRAME STATION 348 STRINGER 5L - 6L IAW SRM 51-30-2. CUT OUT FRAME SECTION IAW DRAWING NR AE727-2-360. FABRICATED AND INSTALLED DO
- [SDR DHL2007748024](https://openairdocs.org/sdr/DHL2007748024.md): Keelbeam · cracked · Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, Keel
  > RAM KEEL BEAM LOWER CHORD CRACKED BS 870. TRIMMED CRACKED AREA OF KEEL BEAM. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SB 727-53-0208 REV 1 MATERIAL USED 0.071" 15-5PH STEEL. HEAT TREATED TO 170-190 KSI PER BRADDOCK METAL SPECS PO NR 7307279 8.75" BY 4" C
- [SDR DHL2007748016](https://openairdocs.org/sdr/DHL2007748016.md): Frame · damaged · Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FORWARD CARGO COMPARTMENT FRAME 640 AREA SHOW SEVERAL FASTENER HOLES IMPROPERLY PERFORMED. BLENDED DAMAGED AREA OF STUB FRAME AT STATION 638 BETWEEN 23L AND 25L. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SIE EO NR SIE-N748DH-10-16-07 MATERIAL USED 0.100"
- [SDR DHL2007748002](https://openairdocs.org/sdr/DHL2007748002.md): Angle · cracked · Oct 18, 2007 · N748DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL STATION 870 RBL 8, VERTICAL ANGLE IS CRACKED. REMOVED AND REPLACED VERTICAL ANGLE IN RIGHT WHEEL WELL STATION 870 RBL 8 IAW B-727 SRM 51-30-5 AND 51-30-2.
- [SDR DHL2007748031](https://openairdocs.org/sdr/DHL2007748031.md): Skin · cracked · Oct 16, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/Skin
  > 2 EACH DENTS HAVE INDICATION OF CRACK HFEC INSPECTION. REMOVED PREVIOUS REPAIR AT FUSELAGE SKIN RIGHT 1342 STRINGER 19R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MATERIAL USED 2024-T3 0.063" PO NR 9005773 DIMENSION 11.5" BY 5.5" IAW B-727 SRM 54-30-3
- [SDR DHL2007748026](https://openairdocs.org/sdr/DHL2007748026.md): Skin · corroded · Oct 16, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/Skin
  > POSSIBLE CORROSION ON SHEAR TIE BS 700 INBOARD OF STRINGER 27R. FABRICATED SKIN DOUBLER REPAIR IAW B-727 SRM 53-30-3 FIGURE 3 AND 53-30-2, AND 2 FRAME SHEAR TIE REPAIR DOUBLERS IAW B-727 SRM 53-10-4 FIGURE 13 AND 14 AT BS 700 STRINGER 27R. MATERIAL USED SKIN
- [SDR DHL2007748030](https://openairdocs.org/sdr/DHL2007748030.md): Shear Tie · cracked · Oct 15, 2007 · N748DH · Boeing 727225 · Fuselage Internal Mounting Structure
  > FORWARD PIT FORWARD SIDE OF FRAME BOTTOM FLANGE AT BS 720 HAS CRACK OUTBOARD OF STRINGER 28R. CUT OUT DAMAGED SECTION AT SHEAR TIE (FRAME) IN FORWARD PIT BS 720 OUTBOARD OF STRINGER 28R IAW B-727 SRM 53-10-4 FIGURE 13 5" BY 2". FABRICATED AND INSTALLED SHEAR
- [SDR DHL2007748017](https://openairdocs.org/sdr/DHL2007748017.md): Frame · dented · Oct 11, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED AT BS 990 JUST ABOVE STRINGER 27L. CUT DAMAGE AREA AT BS 990 ABOVE STRINGER 27L DIMENSION 1" BY.75" IAW B-727 SRM 51-40-3 FIGURE 1. FABRICATED FRAME REPAIR FROM 7075-O PO NR 9004690 DIMENSION 9" BY 4" IAW B-727 SRM 51-40-3 FIGURE 1. HEAT TREAT
- [SDR DHL2007748020](https://openairdocs.org/sdr/DHL2007748020.md): Seat Track · corroded · Oct 9, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN AREA SEAT TRACK CORRODED AT LBL 25 BS 520 TO 690. REMOVED SEAT TRACK SECTION FROM STATION 480 TO 690 LBL 25 IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIGURE 1 AND 53-10-2 FIGURE 7, SPLICE ANGLE REPAIR INSTALLED AT
- [SDR DHL2007748029](https://openairdocs.org/sdr/DHL2007748029.md): Seat Track · corroded · Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO CABIN SEAT TRACK CORRODED AT BS 344 TO 480 RBL 24. REMOVED SEAT TRACK SECTION ON MAIN CARGO CABIN BS 344 TO BS 480 RBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK LOCATED AND DRILLED. MATERIAL USED BAC 1520-792-7178-T6511 PO NR 9005692 DIMENSIO
- [SDR DHL2007748027](https://openairdocs.org/sdr/DHL2007748027.md): Skin · cracked · Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage Main, Plate/Skin
  > 2 EACH DENTS HAVE INDICATION OF CRACKS FROM HFEC INSPECTION. CUT OUT DAMAGED AREA AT RT FUSELAGE SKIN STRINGER 19R BETWEEN BS 1342.4 TO BS 1354.30 IAW SRM 54-30-3 FIGURE 7. FABRICATED DOUBLER REPAIR IAW SRM 54-30-2 FIGURE 4 AND 51-30-2. TREATED AND PRIMED P
- [SDR DHL2007748022](https://openairdocs.org/sdr/DHL2007748022.md): Seat Track · corroded · Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN AREA SEAT TRACK CORRODED AT LBL 45 BS 344 TO 480. REMOVED DAMAGED SECTION OF SEAT TRACK IAW B-727 SRM 51-30-2 FROM STATION 344 TO 480 LBL 45. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW VENTURA AEROSPACE DRAWING NR 2902 MATERIAL USED BAC 1520-7
- [SDR DHL2007748019](https://openairdocs.org/sdr/DHL2007748019.md): Seat Track · corroded · Oct 8, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN AREA SEAT TRACK CORRODED AT BS 500 TO 690 RBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, FABRICATED TWO ANGLES AND FABRICATED STRAP IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED SEAT TRACK PARTS AND AREA IAW SRM 51
- [SDR DHL2007748023](https://openairdocs.org/sdr/DHL2007748023.md): Seat Track · corroded · Oct 5, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED AT BS 480 TO 680 LBL 45. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED 2 NEW SEAT TRACKS, 2 ANGLES AND 1 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS AND SEAT TRACK IAW SR
- [SDR DHL2007748014](https://openairdocs.org/sdr/DHL2007748014.md): Seat Track · corroded · Oct 5, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 950F-1030 RBL 45 HAS CORROSION. REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK, 2 ANGLES AND 2 STRAP IAW SRM 53-10-5 FIGURE 1 AND 51-30-5. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-1
- [SDR DHL2007748021](https://openairdocs.org/sdr/DHL2007748021.md): Seat Track · corroded · Oct 4, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN AREA SEAT TRACK CORRODED AT BS 344-480 LBL 24. REMOVED DAMAGED SEAT TRACK SECTION BS 344-480 LBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM IAW DRAWING NR 2902. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR DHL2007748018](https://openairdocs.org/sdr/DHL2007748018.md): Seat Track · corroded · Oct 3, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED RBL 24 BS 590 TO 689.5. REMOVED SEAT TRACK IAW SRM 53-10-5 FIGURE 1. FABRICATED NEW SEAT TRACK SECTION. FABRICATED 4 ANGLES AND FABRICATED ONE STRAP IAW SRM 53-10-5 FIGURE 1. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2. SEAT
- [SDR DHL2007748015](https://openairdocs.org/sdr/DHL2007748015.md): Seat Track · corroded · Oct 3, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STATION 870 TO 930 LBL45 SEAT TRACK FLANGE HAS CORROSION. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 870 TO 930 LBL45 IAW B-727 SRM 51-30-2. FABRICATED NEW SECTION SEAT TRACK MATERIAL USED BAC 1520-792-7178-T6 DIMENSION 91" IAW B-727 SRM 53-
- [SDR DHL2007748012](https://openairdocs.org/sdr/DHL2007748012.md): Stringer · cracked · Oct 3, 2007 · N748DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > MAIN CABIN STRINGER 15 CRACKED AT BS 720B. CUT OUT DAMAGE AREA DIMENSION CUT OUT IAW SRM 53-10-3 FIGURE 5. FABRICATED REPAIR CHANNEL, FILLER, & TAPERED FILLER IAW SRM 53-10-3 FIGURE 5 AND 51-30-5. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR
- [SDR DHL2007748013](https://openairdocs.org/sdr/DHL2007748013.md): Seat Track · corroded · Oct 2, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 1050-1130 LBL 45 CORRODED. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 1070 TO 1090 LBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION MATERIAL USED BAC 1520-792-7178-T616 PO NR 9005692 DIMENSION 69" LONG, 2 EACH ANGLE MATERIA
- [SDR DHL2007748005](https://openairdocs.org/sdr/DHL2007748005.md): Seat Track · corroded · Oct 2, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STATION 848.95 TO 870 LBL 24 SEAT TRACK FLANGE HAS CORROSION BOTH SIDES. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 848.95 TO 870 LBL 24 IAW B-727 SRM 51-30-2. FABRICATED SECTION SEAT TRACK MATERIAL USED BAC 1520-1466 7178-T6511 PO NR 730788
- [SDR DHL2007748004](https://openairdocs.org/sdr/DHL2007748004.md): Seat Track · corroded · Oct 2, 2007 · N748DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STATION 848.95-870 LBL 45 SEAT TRACK FLANGES HAS CORROSION ON BOTH. REMOVED SECTION OF SEAT TRACK IAW SRM 51-30-2. FABRICATED SECTION SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SECTION SEAT TRA
- [SDR DHL2007748006](https://openairdocs.org/sdr/DHL2007748006.md): Frame · dented · Oct 1, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 540 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 540 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005713 DIMENSION (9.25 BY 4.875") IAW B-727 SRM 53-10-2 FIGURE 3
- [SDR DHL2007748010](https://openairdocs.org/sdr/DHL2007748010.md): Frame · dented · Sep 29, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 580 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 580 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3.
- [SDR DHL2007748003](https://openairdocs.org/sdr/DHL2007748003.md): Frame · dented · Sep 29, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 520 AT STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 520 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005773 DIMENSION 9" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2
- [SDR DHL2007748011](https://openairdocs.org/sdr/DHL2007748011.md): Frame · dented · Sep 28, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 560 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 560 STRINGER 17R IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. DOUB
- [SDR DHL2007748009](https://openairdocs.org/sdr/DHL2007748009.md): Frame · dented · Sep 28, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 600 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 600 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3.
- [SDR DHL2007748008](https://openairdocs.org/sdr/DHL2007748008.md): Frame · dented · Sep 28, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 640 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 640 STRINGER 17R IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. DOUB
- [SDR DHL2007748007](https://openairdocs.org/sdr/DHL2007748007.md): Frame · dented · Sep 28, 2007 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > FRAME DENTED IN MAIN CABIN BS 660 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 660 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2. DOUBLER INS
- [SDR DHL2006748004](https://openairdocs.org/sdr/DHL2006748004.md): Connector · dirty · Oct 24, 2006 · N748DH · Boeing 727225 · Fire Protection System Wiring
  > NR 3 ENGINE FIRE INDICATION ON SHORT FINAL (LIGHT AND BELL) PHASE 1 HEMS COMPLETED FIRE LIGHT WENT OUT WITHOUT BOTTLE DISCHARGE. RESET SYSTEM, CLEANED CONNECTORS ON FIRE LOOP, CHECKED FOR LEAKS ON ENGINE NONE FOUND. PERFORMED TEST PER M/M 26-10-10, OPS CHECK
- [SDR DHL2006748003](https://openairdocs.org/sdr/DHL2006748003.md): Engine · failed · May 7, 2006 · N748DH · Boeing 727225 · Engine (Turbine/Turboprop)
  > NR 2 ENG FAILED AT APPROX 20000 LOUD BANG SHOOK AIRPLANE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.2.
- [SDR DHL2006748002](https://openairdocs.org/sdr/DHL2006748002.md): Fire Detector · malfunctioned · Mar 21, 2006 · N748DH · Boeing 727225 · Fire Detection
  > DURING ROTATION SMOKE AND FIRE DET SYS LIGHTS 4&6 ILLUM WITH AFT FIRE MESSAGE AND LOWER CARGO FIRE LIGHT ILLUM ALONG WITH FIRE BELL. DURING INTL CLIMB LIGHT 4 WENT OUT. THEN 4 MIN AFTER FIRST IND LIGHT 6 WENT OUT AS DID AFT FIRE MESG AND LOWER CARGO FIRE LIG
- [SDR DHL2006748001](https://openairdocs.org/sdr/DHL2006748001.md): Fire Warning · false activation · Feb 1, 2006 · N748DH · Boeing 727225 · Fire Detection
  > LOWER CARGO FIRE WARNING SYSTEM ACTUATED AFTER CHANGING TO SHIPS POWER FROM APU POWER. RESET CCHA & CCHB C/B'S; PERF TEST IAW B727 SMM 26-16-0. NO DEFECTS NOTED. VISUALLY INSP FWD & AFT CARGO BELLY PITS; NO DEFECTS NOTED.
- [SDR DHL2005748001](https://openairdocs.org/sdr/DHL2005748001.md): Light · malfunctioned · Nov 17, 2005 · N748DH · Boeing 727225 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON DURING TEST. REMOVED AND REPLACED EXIT LIGHT ASSY, OPS CK GOOD PER B727 AMM 33-50-101.
- [SDR DHL2005748752](https://openairdocs.org/sdr/DHL2005748752.md): Channel · loose · Sep 16, 2005 · N748DH · Boeing 727225 · Leading Edge Devices
  > NR 1 SLAT HAS PLAY AT ACTUATOR TO SLAT ATTACH POINT. REMOVED CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5070637 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED NEW CHANNEL
- [SDR DHL2005748751](https://openairdocs.org/sdr/DHL2005748751.md): Floorbeam · corroded · Sep 10, 2005 · N748DH · Boeing 727225 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 1166 RBL 36 HAS HEAVY EXFOLIATION ON UPPER FLANGE. CUT OUT DAMAGED AREA OF TOP AFT FLANGE OF FLOORBEAM 4.6 BY 1.0 AT STA 1166 RBL 36 IAW B727 SRM 53-10-8 FIG 8. FAB REPAIR SUPPORT ANGLES FROM 7075T6 PO NR 9001487 22.0 BY 6.0 AND 15.2 BY 6.0 I
- [SDR DHL2005748750](https://openairdocs.org/sdr/DHL2005748750.md): Skin · dented · Sep 8, 2005 · N748DH · Boeing 727225 · Trailing Edge Flaps
  > L/WING I/B AFT FLAP HAS DENT ON UPPER SURFACE I/B END. CUT OUT DENTED AREA ON LT IMB AFT FLAP APPROX 2" DIA FAB FILLER APPROX 2" DIA AND DOUBLER APPROX 5" DIA FROM.012 2024 T3 PO NR 900534 BONDED FILLER AND DOUBLER CURED CLEANED PRIMED AND EALED IAW B727 SRM
- [SDR DHL2005748748](https://openairdocs.org/sdr/DHL2005748748.md): Frame · damaged · Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > BENT FRAME ABOVE STR 17R AT BS 0. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 X 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR B727 SRM 53-10
- [SDR DHL2005748547](https://openairdocs.org/sdr/DHL2005748547.md): Frame · dented · Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > DENT ON FRAME ABOVE STR 17R AT BS 680. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW FRAME REPAIR B727 SRM 53-10-4
- [SDR DHL2005748546](https://openairdocs.org/sdr/DHL2005748546.md): Frame · bent · Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > BENT FRAME ABOVE STR 17R AT BS 660. CUT OUT DAMAGED AREA OF FRAME 1.2 BY 1.7 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B7
- [SDR DHL2005748545](https://openairdocs.org/sdr/DHL2005748545.md): Frame · bent · Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, Frame
  > BENT FRAME ABOVE STR 17R AT BS 640. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B7

Next page: https://openairdocs.org/deregistered/N748DH-2017-10-31/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N748DH' AND deregistration_id = 'N748DH-2017-10-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N748DH-2017-10-31/reports

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