# Service difficulty reports: N937UP, cancelled May 10, 2007

A list on [N937UP, cancelled May 10, 2007](https://openairdocs.org/deregistered/N937UP-2007-05-10.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 · 114 reports

- [SDR UPS04243072](https://openairdocs.org/sdr/UPS04243072.md): Battery · inoperative · Sep 6, 2004 · N937UP · Boeing 72725C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT COME ON WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED BATTERY IN EACH EMERGENCY EXIT LIGHT. OPS CK GOOD REF MM 33-50-01.
- [SDR UPS04242887](https://openairdocs.org/sdr/UPS04242887.md): Spoiler · corroded · Aug 2, 2004 · N937UP · Boeing 72725C · Spoilers
  > RT WING GROUND SPOILER WEB JUST BELOW ACTUATOR HAS CRACK IN LOWER CHORD. REPAIRED.75 INCH CRACK IN L-ANGLE IAW 727 SRM 51-40-04 FIG 1.
- [SDR UPS04241995](https://openairdocs.org/sdr/UPS04241995.md): Fire Loop · out of position · Mar 4, 2004 · N937UP · Boeing 72725C · Fire Detection
  > INSPECTION TYPE:N/A ON CLIMBOUT ENG 1 STRUT OVERHEAT LIGHT ILLUM. CLOSED BLEED AIR SWITCH & PULLED NR 1 BLEED VALVE CB AS PER CHECKLIST. REDUCED THRUST TO IDLE, LIGHT REMAINED ILLUMINATED, OPERATED AT IDLE FOR 3 MIN LIGHT REMAINED ILLUM. SHUT DOWN ENGINE.
- [SDR UPS03241673](https://openairdocs.org/sdr/UPS03241673.md): Overheat Loop · false indication · Dec 29, 2003 · N937UP · Boeing 72725C · Overheat Detection
  > NR 1 ENGINE 1 STRUT OVERHEAD ILLUMINATED IN FLIGHT. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 1 ENG OVERHEAT DETECT LOOPS PER MM 26-14-12. OPS CHECKS GOOD PER MM 26-14-00. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTION BOX FOR PRECAUTION PER MM 26-14-00.
- [SDR UPS03241153](https://openairdocs.org/sdr/UPS03241153.md): Rib · cracked · Aug 15, 2003 · N937UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE: C, RT WING L/E CAVITY SUSPECT CRACK ON RIB ABOVE NR 5 L/E FLAP ACTUATOR ON INVESTIGATION T-SECTION FOUND CRACKED & CORRODED. REPLACED T-SECTION IAW SRM 51-30-02 & DRAWING NR 656268.
- [SDR UPS03241155](https://openairdocs.org/sdr/UPS03241155.md): Structure · cracked · Aug 14, 2003 · N937UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C, CRACK INDICATION FOUND AT BS 910 AFT SIDE OF REINFORCING BEAD RBL 52. REPAIRED IAW EO B727-5310-0088 APPDX C.
- [SDR UPS03241168](https://openairdocs.org/sdr/UPS03241168.md): Shutoff Valve · defective · Aug 12, 2003 · N937UP · Boeing 72725C · Hydraulic System, Main
  > INSPECTION TYPE: C, DURING TEST OF ENG NR 2 HYD SHUTOFF VALVE FAILED TO OPERATE CORRECTLY. TROUBLESHOOTING CARRIED OUT IAW WDM 29-11-01 AND ENG NR 2, SYS A HYD SHUT OFF VALVE FOUND TO BE DEFECTIVE. INSTALLED REPLACEMENT HYD SHUT OFF VALVE IAW MM 29-11-21 RE
- [SDR UPS03241154](https://openairdocs.org/sdr/UPS03241154.md): Fitting · cracked · Aug 12, 2003 · N937UP · Boeing 72725C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C, LT BS 740 FITTING CRACKED BEYOND LIMITS. LT BS 740 FITTING REPLACED IAW UPS EO B727-5310-7477-C.
- [SDR UPS03240021](https://openairdocs.org/sdr/UPS03240021.md): Relay · inoperative · Jan 16, 2003 · N937UP · Boeing 72725C · AC Generation System
  > DURING LANDING ROLLOUT & T/R APPLICATION A PWR LOSS TO THE FLT & ENGINE INSTRUMENTS WAS NOTED. THE COCKPIT WENT MOMENTARILY DARK. APPLIED T/R DURING TAXI IN AND NOTED KW NR 1 JUMPED TO 35 WHILE THE KWNR 2 DROPPED TO ZERO. REMOVED AND REPLACED R58S POWER REL
- [SDR UPS02239930](https://openairdocs.org/sdr/UPS02239930.md): Skin · cracked · Nov 21, 2002 · N937UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:N/A RIGHT INBD AFT FLAP HAS DAMAGE (DENT WITH CRACKED SKIN) JUST OUTBOARD OF INBD CANOE FAIRING. REMOVED DAMAGED SKIN AND CORE, REMOVED INBD AFT FLAP SECTION, REPAIRED FLAP IAW SRM 51-40-20.
- [SDR UPS02239645](https://openairdocs.org/sdr/UPS02239645.md): Light · not seated · Oct 10, 2002 · N937UP · Boeing 72725C · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOPERATIVE. RESEATED FWD ENTRY DOOR EMERGENCY EXIT LIGHT OPERATIONAL CKS GOOD.
- [SDR UPS01236752](https://openairdocs.org/sdr/UPS01236752.md): Flap · delaminated · Aug 31, 2001 · N937UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:W/E RIGHT WING I/B T/E MID-FLAP HAS 3 X 15 INCH DELAMINATION. REMOVED AND REPLACED FLAP IAW MM27-51-03 AND TASK CARD 1 259
- [SDR UPS01234824](https://openairdocs.org/sdr/UPS01234824.md): Control Cable · lack of lube · Feb 1, 2001 · N937UP · Boeing 72725C · Aileron Control System
  > INSPECTION TYPE: IN, AILERON BINDING (REPEAT W/U). TROUBLESHOT PER MM 27-10-00 PAGE 111 INSP CABLE AA & AB NO DEFECT NOTED LUB CABLE, OPS CHECK GOOD.
- [SDR UPS00234489](https://openairdocs.org/sdr/UPS00234489.md): Fitting · broken · Nov 17, 2000 · N937UP · Boeing 72725C · Ailerons
  > INSPECTION TYPE:C, AFTER RIGHT O/B AILERON TAB REMOVAL FOUND O/B FITTING FOR TAB HINGE B-RING BROKEN. REPLACED FITTING IAW DRG 65-21766.
- [SDR UPS00234485](https://openairdocs.org/sdr/UPS00234485.md): Stringer Clip · corroded · Nov 8, 2000 · N937UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, DURING SKIN RETIFACTION WORK AT BS 1180 STRINGER TIE END AT S5L WAS FOUND CORRODED. STRINGER TIE END REPLACED IAW DWG 65-19690 AND SRM 51-30-2.
- [SDR UPS00234452](https://openairdocs.org/sdr/UPS00234452.md): Bushing · cracked · Nov 8, 2000 · N937UP · Boeing 72725C · Engine Mount Section
  > INSPECTION TYPE:C, ENGINE NR 2 MOUNTS LEFT ADAPTER FITTING UPPER LUG LWR BUSH FOUND CRACKED ON FLANGE. BUSHING REPLACED IAW MM 20-10-07 & MM 21-21-12.
- [SDR UPS00234491](https://openairdocs.org/sdr/UPS00234491.md): Support Bracket · cracked · Nov 6, 2000 · N937UP · Boeing 72725C · Landing Gear Doors
  > INSPECTION TYPE:C, RT GEAR MAIN DOOR AFT DOOR STOP LWR SUPPORT BRACKETS CRACKED. REMOVED SUPPORT BRACKETS IAW SRM 21-30-02. ON REMOVAL ATTACH FRAME I/B AND O/B LWR SECTIONS CRACKED. DAMAGED AREA REMOVED IAW SRM 51-10-06. CRACKED AREA REPAIRED IAW SRM 51-20
- [SDR UPS00234478](https://openairdocs.org/sdr/UPS00234478.md): Intercostal · cracked · Nov 6, 2000 · N937UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, INTERCOSTAL BETWEEN FLOORBEAM BS 294.5 TO BS 312R CRACKED RBL 46 APPR OX. STOP DRILLED CRACK ON INTERCOSTAL BETWEEN BS 294.5 & 312 RBL 46 APPROX IAW SRM 51-40-03, 51-10-01. HFEC C/O POST STOP DRILL IAW B727 NDTM PT6 51-00-00 FIG 4. CRACK
- [SDR UPS00234453](https://openairdocs.org/sdr/UPS00234453.md): Stringer · cracked · Nov 6, 2000 · N937UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, TO FACILITATE ACCESS TO FASTENERS IN AREA AT BS 1183 AND STR 4L REMOVAL OF STRINGER END IS REQD, ON REMOVAL OF STRINGER IT WAS FOUND TO BE CRACKED. REPAIR CARRIED IAW SRM 51-30-2 SRM 53-11-00 & MM 20-50-1.
- [SDR UPS00234488](https://openairdocs.org/sdr/UPS00234488.md): Frame · cracked · Nov 5, 2000 · N937UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE:C, CRACK BS 910 FRAME RT W/WELL. REPAIRED CRACK AT BS 910 FRAME IAW EO B727-5310-1896B.
- [SDR UPS00234497](https://openairdocs.org/sdr/UPS00234497.md): Frame · cracked · Nov 4, 2000 · N937UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE:C, BS 930 FRAME IN LT WHEEL WELL HAS SUSPECT CRACKS BETWEEN THE FASTENER HOLES AT AFT FLANGE. CRACKS CONFIRMED. AREA REPAIRED IAW UPS EO B727-5310-2611 AND SMRO EO 2000-041-005, UPS ENG FILE NUMBER 727-53-2301.
- [SDR UPS00234495](https://openairdocs.org/sdr/UPS00234495.md): Casting · cracked · Nov 4, 2000 · N937UP · Boeing 72725C · Landing Gear Doors
  > INSPECTION TYPE:C, RIGHT MAIN GEAR WING DOOR AFT HINGE CASTING CRACKED IN TWO PLACES. RT WING DOOR REPLACED IAW MM 32-12-11 AND ADJ/TESTED IAW 32-12-11.
- [SDR UPS00234493](https://openairdocs.org/sdr/UPS00234493.md): Frame · cracked · Nov 4, 2000 · N937UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE:C, BS 930 FRAME IN LT WHEEL WELL HAS SUSPECT CRACKS BETWEEN FASTENER HOLES AT AFT FLANGE. REPAIR CARRIED OUT IAW SMRO EO 2000-041-005 UPS ENGINEERING FILE NO 727-53-2301.
- [SDR UPS00234477](https://openairdocs.org/sdr/UPS00234477.md): Stringer · corroded · Nov 4, 2000 · N937UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, CORROSION ON STR 21R AT BS 480. REPAIRED IAW SRM 53-10-3 FIG 1.
- [SDR UPS00234476](https://openairdocs.org/sdr/UPS00234476.md): Stringer · corroded · Nov 4, 2000 · N937UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C, CORROSION ON STR 24R AT BS 470. REPAIRED STR 24R AT BS 470 IAW SRM 53-10-3 FIG 1.
- [SDR UPS00234487](https://openairdocs.org/sdr/UPS00234487.md): Door Frame · cracked · Nov 3, 2000 · N937UP · Boeing 72725C · Fuselage Main, Structure
  > INSPECTION TYPE:C, AFT CARGO DOOR FWD FRAME BENEATH NR 1 STOP FITTING CRACKED. REPLACED LWR FORWARD FRAME ON AFT CARGO DOOR IAW SRM 51-30-2 AND DRAWING 65-18625.
- [SDR UPS00234480](https://openairdocs.org/sdr/UPS00234480.md): Frame · cracked · Nov 3, 2000 · N937UP · Boeing 72725C · Fuselage Main, Frame
  > INSPECTION TYPE:C, SUSPECT CRACK BS 950L AT FWD LUG OF SWING LINK ON 950 FRAME. HFEC INSPECTION C/O ON ABOVE LUG IAW B727 NDTM PT6 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REPAIR C/O PER SMRO EO 2000-041-004. UPS FILE 727-53-2296.
- [SDR UPS00234481](https://openairdocs.org/sdr/UPS00234481.md): Web · corroded · Nov 2, 2000 · N937UP · Boeing 72725C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON LT AT BS 312 APPROX VERTICAL WEB OF TORQUE BOX. VERTICAL WEB FOUND TO BE CRACKED BEYOND LIMITS IAW SRM 51-10-10. REPLACED VERTICAL WEB 65-18415-49 IAW DRW 65-18415 AND SRM 51-30-3. TO AID WITH REPLACEMENT OF VERTICAL WEB 65-1
- [SDR UPS00234492](https://openairdocs.org/sdr/UPS00234492.md): Fitting · cracked · Nov 1, 2000 · N937UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:C, RIGHT O/B FLAP O/B JACKSCREW FAIRING LWR ATTACH FITTING IS CRACKED AND SEVERAL FASTENERS ARE LOOSE AT UPPER ATTACH POINT. FITTING INSTALLED AND LOOSE FASTENERS REPLACED IAW SRM 51-30-2.
- [SDR UPS00234490](https://openairdocs.org/sdr/UPS00234490.md): Fitting · cracked · Nov 1, 2000 · N937UP · Boeing 72725C · Trailing Edge Flaps
  > INSPECTION TYPE:C, SUSPECT CRACK ON O/B AFT NR 3 TRAP TRACK SUPPORT FITTING ATTACH TO SPOILER SUPPORT BEAM AT BARREL NUT HOLE. REMOVED FITTING IAW SRM 51-31-00 AND INSTALLED FITTING IAW SRM 51-30 -02.
- [SDR UPS00234486](https://openairdocs.org/sdr/UPS00234486.md): Skin · cracked · Nov 1, 2000 · N937UP · Boeing 72725C · Spoilers
  > INSPECTION TYPE:C, RT WING T/E UPPER AT NR 12 SPOLIER CTRL I/B HINGE SKIN CRACKED. SKIN REPAIRED IAW 57-30-4.
- [SDR UPS00234482](https://openairdocs.org/sdr/UPS00234482.md): Lap Joint · corroded · Nov 1, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION AT LAP JOINT S19R BS 500 - 481 AT VARIOUS LOCATIONS. LFEC INSP OF LAP JOINT BS 440 - 520 S19R IAW B727 NDTM. RESULT 15 - 20 PERCENT CORROSION. OTHER AREAS NDF. HFEC INSP LAP JOINT IAW B727 NDTM NO DEFECTS FOUND. REPAIR CARRIED
- [SDR UPS00234475](https://openairdocs.org/sdr/UPS00234475.md): Mount · corroded · Nov 1, 2000 · N937UP · Boeing 72725C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 3 FWD MOUNT, PITTING CORROSION IN ALL 4 MOUNT HOLES. REPAIR C/O IAW EO B727-5440-11592 APP B.
- [SDR UPS00234474](https://openairdocs.org/sdr/UPS00234474.md): Mount · corroded · Nov 1, 2000 · N937UP · Boeing 72725C · Engine Mount Section
  > INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT, PITTING CORROSION IN AFT I/B HOLE. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592 APP B.
- [SDR UPS00234473](https://openairdocs.org/sdr/UPS00234473.md): Cowling · chafed · Nov 1, 2000 · N937UP · Boeing 72725C · Engine Cowling System
  > INSPECTION TYPE:C, ENGINE NR 1 NOSE COWL EXTERNAL SKIN WORN DUE CHAFING OFF PYLON NOSE. NOSE COWL REPAIRED IAW SMRO EO 2000-041-001 UPS FILE 727-71-0095.
- [SDR UPS00234472](https://openairdocs.org/sdr/UPS00234472.md): Skin · corroded · Nov 1, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION AT LAP JOINT S19R BS 500 TO BS 481 AT VARIOUS LOCATIONS. HFEC AND LFEC CARRIED OUT LFEC FOUND 15 - 20 PERCENT CORROSION BS 485 - 498. OTHER AREAS NO DEFECTS FOUND. HFEC RESULTS NO DEFECTS FOUND. FASTENERS REMOVED IN CRITICAL AR
- [SDR UPS00234454](https://openairdocs.org/sdr/UPS00234454.md): Skin · corroded · Nov 1, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1180 S4L. REPAIRED AREA FROM BS 1163 - 1183 IAW SRM 53-30-3 FIG 14.
- [SDR UPS00234449](https://openairdocs.org/sdr/UPS00234449.md): Bracket · cracked · Nov 1, 2000 · N937UP · Boeing 72725C · Cargo/Baggage Doors
  > INSPECTION TYPE:C, FWD CARGO DOOR NET SUPPORT BRACKET CRACKED AT AFT END. CRACK REPAIRED IAW SRM 51-40-2.
- [SDR UPS00234479](https://openairdocs.org/sdr/UPS00234479.md): Skin · cracked · Oct 31, 2000 · N937UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:C, NR 5 KRUEGER FLAP INNER SKIN CRACKED JUST I/B OF ACTUATOR X2. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC C/O IAW B727 NDTM PT.6 51-0 0-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN STOP DRILL HOLE. REPAIR C/O IAW EO B727-5750-3082.
- [SDR UPS00234455](https://openairdocs.org/sdr/UPS00234455.md): Skin · corroded · Oct 31, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION ON SKIN AT BS 1140 BETWEEN STR 3R AND STR 4R. AREA REPAIRED FROM BS 1140 - BS 1160 IAW SRM 53-30-3.
- [SDR UPS00234484](https://openairdocs.org/sdr/UPS00234484.md): Skin · cracked · Oct 30, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CRACK IN SKIN AT L/WING ICE LIGHT UPPER FWD CUTOUT. CRACK STOP DRILLED IAW SRM 51-10-01. HFEC INSP C/O ON ABOVE AREA IAW B727 NDTM PT.6 FIG 4. RESULT: CRACK CONTAINED WITHIN STOP DRILL. AREA REPAIRED IAW SRM 53-30-3 FIG 22 AND SMRO EO 20
- [SDR UPS00234483](https://openairdocs.org/sdr/UPS00234483.md): Skin · corroded · Oct 30, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 475 BETWEEN S7L AND S6L. REPAIR C/O IAW SMRO EO 2000-041-006. UPS EO B727-5330-13568.
- [SDR UPS00234456](https://openairdocs.org/sdr/UPS00234456.md): Skin · corroded · Oct 30, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, CORROSION AT VARIOUS MARKED LOCATIONS S4L LWR SKIN BETWEEN BS 750 AND BS 870. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 14.
- [SDR UPS00234450](https://openairdocs.org/sdr/UPS00234450.md): Skin · cracked · Oct 30, 2000 · N937UP · Boeing 72725C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CRACK FROM FASTENER HOLE IN SKIN AT NR 3 RT COCKPIT WINDOW AFT VERTICAL CUT OUT. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 8.
- [SDR UPS00233343](https://openairdocs.org/sdr/UPS00233343.md): Valve · inoperative · Jul 11, 2000 · N937UP · Boeing 72725C · Cabin Pressure Control System
  > INSPECTION TYPE:N/A, AIRCRAFT WILL NOT MAINTAIN PRESSURIZATION. REMOVED AND REPLACED RIGHT PACK FLOW SENSING VENTURA VALVE IAW DC8 MM 21-51-62, OPS CHECKS GOOD. (P/N 106892-1-1) (S/N P-501) ON, (S/N P-444) OFF.
- [SDR UPS00232077](https://openairdocs.org/sdr/UPS00232077.md): Stringer · cracked · Mar 18, 2000 · N937UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, STRINGER 24 RT CRACKED AT BS 290. INSTALLED STRINGER REPAIR IN ACCORDANCE WITH B727 SRM 53-10-3 FIG 1.
- [SDR UPS00232078](https://openairdocs.org/sdr/UPS00232078.md): Stringer · cracked · Mar 17, 2000 · N937UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, CORRODED AND CRACKED STRINGER 24 RT LAP JOINT STA 296 UPPER OUTER SKIN. INSTALLED LAP SKIN REPAIR IN ACCORDANCE WITH UPS EO B727-5330-0509 A PPENDIX 8.3
- [SDR UPS99229484](https://openairdocs.org/sdr/UPS99229484.md): Bracket · cracked · Apr 29, 1999 · N937UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:SI, CRACKED NR 6 K-FLAP ACTUATOR I/B MOUNT BRACKET, LWR FWD RADIUS. FABRICATED AND REPLACED MOUNT BRACKET PER SRM 51-20-1.
- [SDR UPS99229483](https://openairdocs.org/sdr/UPS99229483.md): Skin · cracked · Apr 29, 1999 · N937UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:SI, CRACK RUNNING FROM NR 6 SLAT O/B GUIDE HOOK MOUNT HOLE TO O/B RIVET HOLE. REMOVED AND REPLACED NR 6 SLAT PER MM 27-81-11.
- [SDR UPS99229482](https://openairdocs.org/sdr/UPS99229482.md): Rib · cracked · Apr 29, 1999 · N937UP · Boeing 72725C · Leading Edge Devices
  > INSPECTION TYPE:SI, NR 4 SLAT RIB CRACKED AT ACTUATOR ROD END BOLT O/B SIDE. REPLACED RIB PER SRM 51-30-5.

Next page: https://openairdocs.org/deregistered/N937UP-2007-05-10/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 = 'N937UP' AND deregistration_id = 'N937UP-2007-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N937UP-2007-05-10/reports

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